An Investigation of the Characteristics of the NACA RM-10 (with and Without Fins) in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.9
1954-11-26
Miscellaneous
No indication
English
Investigation of two-step nozzle in Langley 11-inch hypersonic tunnel
| Engineering Index Backfile | 1950
The Langley 15-inch Mach 6 High Temperature Tunnel
| AIAA | 1992
Liquefaction of air in the Langley 11-inch hypersonic tunnel
| TIBKAT | 1954